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1.
  • Silfverskiöld, Stefan, 1964-, et al. (author)
  • Technology Forecast 2017 - Military Utility of Future Technologies : A Report from Seminars at the Swedish Defence University’s (SEDU) Military-Technology Division
  • 2017
  • Reports (other academic/artistic)abstract
    • Two technology forecast reports from the Fraunhofer Institute, three reports from the Swedish Defence Research Institute (FOI) and two publications from the Massachusetts Institute of Technology (MIT) have been reviewed by staff at the Military-Technology Division at the Swedish Defence University (SEDU). The task given by the Defence Material Administration (FMV) was to assess the military utility of the given technologies in a time frame to up 2040, from a Swedish Armed Forces (SwAF) perspective.In the review we assessed the military utility of certain technologies as possible contributions to the operational capabilities of the SwAF, based on identified and relevant scenarios. Because a new capability catalogue is under development at the SwAF Headquarters, this report only presents general assessments of the capability impact of the technologies studied.The technologies were grouped into four classes: potentially significant, moderate, negligible, or uncertain military utility.The classification uncertain military utility was given to technologies that are difficult to put in the other three classes, it was not because the technology readiness level (TRL) will not bereached by 2040.The following technologies were assessed to have the potential for significant military utility:- Nanocarbons for photonic applicationsThe following technologies were assessed to have a potential for moderate military utility;- Internet of things (IoT)- Materials and technologies for protection against chemical agentsThe following technologies were assessed to have uncertain military utility;- Post-quantum cryptography- New applications for hyperspectral image analysis for chemical and biological agentsNo technology was found to have negligible military utility.The method used in this technology forecast report was to assign each report to one reviewer in the working group. Firstly, each forecast report was summarized. The Fraunhofer assessment of technical readiness level (TRL) in the time period was held to be correct. Each technology was then put into one or more scenarios that were assessed to be suitable for assessing the military utility as well as indicating any possibilities and drawbacks. Based on a SWOTanalysis, the assessed contributions to the fundamental capabilities, and to the factors DOTMPLFI (Doctrine, Organization, Training, Materiel, Leadership, Personnel, Facilities and Interoperability), were listed. Furthermore, the expected SwAF R&D requirements, to facilitate the introduction of the technology are given. The Military utility was assessed using a model developed by the Military-Technology Division. Finally, conclusions and an overall rating of the potential military utility of each technology were presented.The chosen definition of military utility clearly affects the result of the study. The definition used here (“the military utility of a certain technology is its contribution to the operational capabilities of the SwAF, within identified relevant scenarios”) has been used in our Technology Forecasts since 2013.Our evaluation of the method used shows that there is a risk that assessments can be biased by the participating experts’ presumptions and experience from their own field of research. It should also be stressed that the seven technologies’ potential military utility was assessed within the specific presented scenarios and their possible contribution to operational capabilities within those specific scenarios, not in general. When additional results have been found in the analysis, this is mentioned.The greatest value of the method used is its simplicity, cost effectiveness and that it promotes learning within the working group. The composition of the working group and the methodology used are believed to provide a broad and balanced coverage of the technologies being studied. This report should be seen as an executive summary of the research reports and the intention is to help the SwAF Headquarters to evaluate the military utility of emerging technologies within identified relevant scenarios.Overall, the research reports are considered to be balanced and of high quality in terms of their level of critical analysis regarding technology development. These reports are in line with our task to evaluate the military utility of the emerging technologies.
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  • Sturesson, Peter, 1981- (author)
  • Sense, Actuate and Survive : Ceramic Microsystems for High-Temperature Aerospace Applications
  • 2018
  • Doctoral thesis (other academic/artistic)abstract
    • In aerospace applications, but also in manufacturing, mining, energy industry and natural hazards, high temperature, corrosion, erosion and radiation, challenge the performance and being of hardware.In this work, high-temperature co-fired ceramic (HTCC) alumina and platinum have been used for a range of devices intended for aerospace applications at up to 1000°C.The thermomechanics of a pressure sensor was investigated, and the interfacing was attained by wireless powering and reading. However, read range was limited and sensitivity decreased with temperature. Silver, electroplated after sintering, was found to remedy this until it eventually alloyed with platinum.Copper was electroplated and oxidized for oxygen storage in a microcombustor, intended for sample preparation for optogalvanic spectroscopy (OGS) to indicate extraterrestrial life. Despite delamination, caused by residual stresses, the device operated successfully.Conversely, pre-firing metallization by integration of platinum wires was studied. Freely suspended, and despite heat-induced shape irregularities, these were found advantageous over screen printed elements for gas heating, and temperature and pressure sensing. By fusing off the wires, spherical tips, allowing for impedance monitoring of microplasma sources in, e.g., OGS, were formed.Microplasma sources can also be used for gas heating. This, together with screen printed and suspended resistive heaters, was evaluated in a microthruster, showing that plasma heating is the most effective, implying fuel consumption reduction in satellite propulsion.In conclusion, HTCC alumina microdevices are thermally stable and could benefit several aerospace applications, especially with the complementary metallization schemes devised here.Future developments are expected to include both processing and design, all with the intention of sensing, actuating and surviving in high-temperature environments.
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  • Lundmark, Martin, 1963-, et al. (author)
  • Technology Forecast 2018 : Military Utility of Future Technologies
  • 2018
  • Reports (other academic/artistic)abstract
    • SummaryFour technology forecast reports from the Fraunhofer Institute and two reports from the Swedish Defence Research Agency (FOI) have been reviewed by staff at the Military Technology Division at the Swedish Defence University (SEDU). The task given by the Defence Materiel Administration (FMV) was to assess the military utility of the given technologies in a timeframe up to the year 2040, from a Swedish Armed Forces (SwAF) perspective.In the review, we assess the military utility of certain technologies as possible contributions to the operational capabilities of the SwAF, based on identified and relevant scenarios.The technologies are grouped into four classes of military utility: potentially significant, moderate, negligible or uncertain.The following technologies were assessed to have the potential for significant military utility:Rapid field      identification of harmful microorganismsHypersonic      propulsion The following technologies were assessed to have a potential for moderate military utility:Non-line-of-sight      imagingArtificial      intelligence for military decision support The following technologies were assessed to have uncertain military utility:Structural      energy storageTriboelectric      nanogenerators No technology was found to have negligible military utility.The method used in this technology forecast report was to assign each report to one reviewer in the working group. Firstly, each forecast report was summarized. A new methodological step this year was for each reviewer to discuss the assigned technologies with researchers from FOI. This proved to be a valuable enhancement for understanding the technologies’ present state and likely future development.The chosen definition of military utility clearly affects the result of the study. The definition used here, ‘the military utility of a certain technology is its contribution to the operational capabilities of the SwAF, within identified relevant scenarios’ has been used in our Technology Forecasts since 2013.Our evaluation of the method used shows that there is a risk that assessments can be biased by the participating experts’ presumptions and experience from their own field of research. It should also be stressed that the six technologies’ potential military utility was assessed within the specific presented scenarios and their possible contribution to operational capabilities within those specific scenarios, not in general. When additional results have been found in the analysis, this is mentioned.The greatest value of the method used is its simplicity, cost effectiveness and that it promotes learning within the working group. The composition of the working group and the methodology used are believed to provide a broad and balanced coverage of the technologies being studied. This report should be seen as an executive summary of the research reports and the intention is to help the SwAF Headquarters to evaluate the military utility of emerging technologies within identified relevant scenarios.Overall, the research reports are considered to be balanced and of high quality in terms of their level of critical analysis regarding technology development. These reports are in line with our task to evaluate the military utility of the emerging technologies.
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  • Seton, Ragnar, 1985-, et al. (author)
  • Investigating the plasma properties of a Xe-microplasma thruster
  • 2019
  • In: Journal of Physics, Conference Series. - : Institute of Physics (IOP). - 1742-6588 .- 1742-6596. ; 1319
  • Journal article (other academic/artistic)abstract
    • By combining optical emission spectroscopy (OES) and Langumuir probes, the plasma properties of a Xenon-microplasma thruster have been investigated. Using IV-curve analysis the properties of the plasma have been determined and correlated to the power fed into it. Satisfactory agreement has been obtained with the results of OES measurements (line-ratio technique) and shock-cell distance calculations. While the fuel consumption of the thruster decreased very linearly with the power fed to the plasma, the plasma properties was found to have behave in a more complex way. In the studied power range, the density ratio between at least two ions, with upper configurations 5p5(2P◦3/2)7p and 5p5(2P◦3/2)6p, strongly indicated that the ionization processes of the former was favorable in terms of thrust for the geometry of the nozzle. This was supported electron temperature measurements from IV-curves. 
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  • Sturesson, Peter, 1981-, et al. (author)
  • Ceramic Pressure Sensor for High Temperatures – Investigation of the Effect of Metallizationon on Read Range
  • 2017
  • In: IEEE Sensors Journal. - 1530-437X .- 1558-1748. ; 17:8, s. 2411-2421
  • Journal article (peer-reviewed)abstract
    • A study on the relationship between circuit metallization, made by double-layer screen printing of platinum and electroplating of silver on top of platinum, and its impact on practical read range of ceramic LC resonators for high-temperature pressure measurements is presented. Also included is the first realization of membranes by draping a graphite insert with ceramic green body sheets. As a quality factor circuit reference, two-port microstrip meander devices were positively evaluated and to study interdiffusion between silver and platinum, test samples were annealed at 500 degrees C, 700 degrees C, and 900 degrees C for 4, 36, 72, and 96 h. The LC resonators were fabricated with both metallization methods, and the practical read range at room temperature was evaluated. Pressure-sensitive membranes were characterized for pressures up to 2.5 bar at room temperature, 500 degrees C and up to 900 degrees C. Samples electroplated with silver exhibited performance equal to or better than double-layer platinum samples for up to 60 h at 500 degrees C, 20 h at 700 degrees C, and for 1 h at 900 degrees C, which was correlated with the degree of interdiffusion as determined from cross-sectional analysis. The LC resonator samples with double-layer platinum exhibited a read range of 61 mm, and the samples with platinum and silver exhibited a read range of 59 mm. The lowest sheet resistance, and, thereby, the highest read range of 86 mm, was obtained with a silver electroplated LC resonator sample after 36 h of annealing at 500 degrees C.
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  • Sturesson, Peter, 1981-, et al. (author)
  • Effect of Resistive and Plasma Heating on the Specific Impulse of a Ceramic Cold Gas Thruster
  • 2019
  • In: Journal of microelectromechanical systems. - 1057-7157 .- 1941-0158. ; 28:2, s. 235-244
  • Journal article (peer-reviewed)abstract
    • The research and development of small satellites has continued to expand over the last decades. However, the propulsion systems with adequate performance have persisted to be a great challenge. In this paper, the effects of three different heaters on the specific impulse and overall thrust efficiency of a cold gas microthruster are presented. They consisted of a conventional, printed resistive thick-film element, a freely suspended wire, and a stripline split-ring resonator microplasma source, and were integrated in a single device made from the high-temperature co-fired ceramics. The devices were evaluated in two setups, where the first measured thrust and the other measured shock cell geometry. In addition, the resistive elements were evaluated as gas temperature sensors. The microplasma source was found to provide the greatest improvement in both specific impulse and thrust efficiency, increasing the former from an un-heated level of 44–56 s when heating with a power of 1.1 W. This corresponded to a thrust efficiency of 55%, which could be compared with the results from the wire and printed heaters which were 51s and 18%, and 45s and 14%, respectively. The combined results also showed that imaging the shock cells of a plasma heated thruster was a simple and effective way to determine its performance, when compared to the traditional thrust balance method.
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10.
  • Sturesson, Peter, 1981-, et al. (author)
  • Fabrication of Suspended All-Metal Sensor Elements in Ceramic Laminates
  • 2016
  • In: Proc. of Micronano System Workshop 2016, Lund, Sweden, May 17-18, 2016.
  • Conference paper (other academic/artistic)abstract
    • To target a wide range of high-temperature applications [1-4], the Ångström Space Technology Centre has added High-Temperature Co-fired Ceramics, HTTC, technology to its repertoire. Usually, this technology follows a processing scheme where thin sheets of green-body ceramics are metallized through screen printing and structured by embossing, punching or milling, before they are laminated and sintered to form components. A limitation with this, is the difficulty of realizing freely suspended metal structures, which is a disadvantage in, e.g., the fabrication of calorimetric sensors or electric field probes. In this work, the embedding of platinum wires in HTCC is explored experimentally, and demonstrated for use in pressure and plasma I-V sensing.
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